System Performance

• Performance to LEO (expected):
• 400 lbs to 270 nm, 28.5° inclination
• Nonlinear Finite Element Analysis
• 250 lbs to 270 nm, 97.1° inclination

MIPCC Powered Vehicle (MPV)

• New aircraft design
• 81 ft span, 89 ft length, 2700 ft2 wing area
• 90,000 lb GTOW
• 4 F100-class engines with LOX/Water MIPCC

Expendable Rocket Vehicle (ERV)

• 2 stage Vehicle, 16,000 lbs at release
• 1st Stage: Hybrid Rocket Motor
• 2nd Stage: Solid Rocket Motor
• Payload volume: 10 ft length, 6 ft diameter

RASCAL Phase II Contractors
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